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| Experimental study of the high-power laser resistance of ablative material-filled sandwich panels with truss cores under hypersonic airflow 期刊论文
COMPOSITE STRUCTURES, 2022, 卷号: 301, 页码: 116139
作者: Yuan W(袁武); Wang JT(王江涛) ; Wang RX(王睿星); Wang Z(王喆); Song HW(宋宏伟); Huang CG(黄晨光)
 Adobe PDF(9765Kb) |  收藏 | 浏览/下载：180/44 | 提交时间：2022/10/23
Sandwich panel Thermal insulation Lightweight structure Failure point |
| Parameters for evaluating the efficiency of inlet compression 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 12, 页码: 51-56
作者: Chen KT(陈科挺); Yue LJ(岳连捷); Zhang XY(张新宇)
Adobe PDF(511Kb) | 收藏 | 浏览/下载：197/37 | 提交时间：2022/01/12
Airbreathing engine Compression efficiency Compression quality Inlet Self-consistency |
| Existence of positive skewness of velocity gradient in early transition 期刊论文
PHYSICAL REVIEW FLUIDS, 2021, 卷号: 6, 期号: 10, 页码: 21
作者: Zhao HK; Liu YW; Shao L; Fang L; Dong M(董明)
Adobe PDF(4359Kb) | 收藏 | 浏览/下载：187/28 | 提交时间：2022/01/12 |
| Characteristics of wall-shear stress fluctuations in shock wave and turbulent boundary layer interaction 期刊论文
JOURNAL OF TURBULENCE, 2021, 页码: 23
作者: Tong FL(童福林); Duan JY(段俊亦); Li XL(李新亮)
Adobe PDF(5190Kb) | 收藏 | 浏览/下载：234/60 | 提交时间：2021/11/01
Wall-shear stress shock wave turbulent boundary layers |
| Optical diagnostics in a detonation-driven direct-connected circular combustor fueled with hydrogen for mach 10 scramjet 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2021, 卷号: 46, 期号: 54, 页码: 27801-27815
作者: Zhou GX(周功喜); Zhang X(张旭); Li JP(李进平); Zhang XY(张晓源); Zhang SZ(张仕忠); Lin X(林鑫); Li F(李飞); Chen H(陈宏); Yue LJ(岳连捷); Yu XL(余西龙)
Adobe PDF(4108Kb) | 收藏 | 浏览/下载：329/47 | 提交时间：2021/09/07
High mach number scramjet Circular cross-section TDLAS Multi-view simultaneous imaging POD |
| Direct numerical simulation of impinging shock wave and turbulent boundary layer interaction over a wavy-wall 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 5, 页码: 350-363
作者: Tong FL(童福林); Sun D(孙栋); Li XL(李新亮)
Adobe PDF(4402Kb) | 收藏 | 浏览/下载：193/43 | 提交时间：2021/06/07
Direct numerical simulation Low-frequency unsteadiness Shock waves Turbulent boundary layer Wavy-wall |
| Flow structure of pressure transmission tube and its influence on unsteady pressure measuring results in compressible flow 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 108, 页码: 22
作者: Tong XT(仝晓通); Zhang QF(张启帆); Yue LJ(岳连捷); Zhang XY(张新宇)
Adobe PDF(8067Kb) | 收藏 | 浏览/下载：376/61 | 提交时间：2021/03/03
Unsteady pressure measurement Pressure sensor Pressure transmission tube Dynamic response Compressible flow |
| Impulse force-measurement system 期刊论文
SHOCK WAVES, 2020, 页码: 11
作者: Wang YP(汪运鹏); Jiang ZL(姜宗林)
Adobe PDF(1551Kb) | 收藏 | 浏览/下载：236/65 | 提交时间：2020/11/30
Shock tunnel High enthalpy Aerodynamic force measurement Strain gauge balance |
| Investigation on rod-airfoil noise with high-order cell-centered finite difference method and acoustic analogy 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 102, 页码: 22
作者: Jin Y; Liao F(廖飞); Cai JS; Morris PJ
Adobe PDF(7457Kb) | 收藏 | 浏览/下载：240/87 | 提交时间：2020/07/06
Aeroacoustics Rod-airfoil configuration Cell-centered finite difference method Delayed detached eddy simulation FW-H acoustic analogy |
| Experimental Investigation of Hypervelocity Flow in an Expansion Tunnel 期刊论文
AIAA JOURNAL, 2020, 卷号: 58, 期号: 6, 页码: 2776-2783
作者: Yuan CK(苑朝凯); Zhou K(周凯); Hu ZM(胡宗民); Liu YF(刘云峰); Jiang ZL(姜宗林)
Adobe PDF(1471Kb) | 收藏 | 浏览/下载：232/57 | 提交时间：2020/07/06 |
